FENGYUN 1C DEB, 30525
Orbit data source: Space-Track
FENGYUN 1C DEB, 30525 is space debris in SSO originally from a launch on Mon, 10 May 1999 UTC launched from the Taiyaun Space Center, China (TSC). Fengyun 1C debris stems from the Chinese weather satellite Fengyun-1C, which was intentionally destroyed by a Chinese anti-satellite missile in 2007. This event dramatically increased the amount of space debris, with thousands of trackable fragments posing hazards to satellites and human spaceflight. The Fengyun 1C debris cloud has become a focal point in discussions about space sustainability and the need for international regulations to prevent the creation of new debris.
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30525 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown shape, 0.1 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 22 hours ago
TLE from 22 hours ago
0 FENGYUN 1C DEB
1 30525U 99025AJP 26259.08401343 .00000874 00000-0 93479-3 0 9991
2 30525 98.5800 115.4555 0292367 305.0544 52.3491 13.59276786968846Epoch: 2026-09-16T02:00Z
TLE epoch observation values (Epoch: 2026-09-16T02:00:58.760Z)
Latitude
-0.00005°
Longitude
90.16999°
Altitude
912.767 km
Speed
7.459 km/s
True Right ascension
07h 41m 49s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
16:37:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,252.304 km
Perigee altitude
818.801 km
Semi-major axis
7,413.689 km
Eccentricity
0.02924
Inclination
98.58°
RAAN
115.4555°
Arg. of periapsis
305.0544°
True anomaly
55.06117°
Mean anomaly
52.3491°
Eccentric anomaly
53.69913°
Mean motion
3.4001 °/min
Orbital period
105.88 mins
BSTAR
0.00093479
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Other satellites on launch #25 in the year 1999 (1999-05-10 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.FENGYUN 1C DEB Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-09-17 01:38:23.990Z | 58.654° ENE | 2026-09-17 01:41:23.990Z | 83.963° E | 15.439° | 2026-09-17 01:45:23.990Z | 118.057° SE |
| 13 mins | 2026-09-17 03:21:23.990Z | 14.854° NNE | 2026-09-17 03:27:23.990Z | 157.268° SSE | 83.478° | 2026-09-17 03:34:23.990Z | 193.477° SSW |
| 8 mins | 2026-09-17 05:07:23.990Z | 333.069° NNW | 2026-09-17 05:10:23.990Z | 305.137° NW | 20.354° | 2026-09-17 05:15:23.990Z | 260.742° W |
| 10 mins | 2026-09-17 13:29:23.990Z | 119.633° SE | 2026-09-17 13:33:23.990Z | 70.747° E | 33.866° | 2026-09-17 13:39:23.990Z | 5.118° NNE |
| 11 mins | 2026-09-17 15:13:23.990Z | 199.846° SSW | 2026-09-17 15:18:23.990Z | 270.249° WNW | 41.045° | 2026-09-17 15:24:23.990Z | 332.675° NNW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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